SYSTEMS AND METHODS FOR CONTROLLING AN ELECTRIC VERTICAL TAKE-OFF AND LANDING AIRCRAFT

A method of controlling an electric aircraft that has a plurality of actuators that includes a plurality of electric propulsion units includes: receiving force and moment commands for the electric aircraft; determining control commands for the plurality of actuators based on the desired force and mo...

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Bibliographische Detailangaben
Hauptverfasser: CHEN, Alan, XUE, Nansi, GOLDMAN, Benjamin, DEPENBUSCH, Nathan, BOWER, Geoffrey, C
Format: Patent
Sprache:eng ; fre ; ger
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